火炸药学报
火炸藥學報
화작약학보
CHINESE JOURNAL OF EXPLOSIVES & PROPELLANTS
2009年
3期
29-34
,共6页
爆炸力学%子母式战斗部%偏心起爆%中心起爆%数值模拟%速度增益
爆炸力學%子母式戰鬥部%偏心起爆%中心起爆%數值模擬%速度增益
폭작역학%자모식전두부%편심기폭%중심기폭%수치모의%속도증익
explosion mechanics%deformable warhead%non-center detonation%center detonation numericalsimulation%velocity gain
为研究偏心起爆子母式战斗部破片速度的增益,运用LS-DYNA对子母式定向战斗部变形和爆轰驱动破片飞散过程进行了数值模拟,模拟结果与试验结果吻合.结果表明,与中心起爆相比,在与起爆位置相对的方向上,偏心起爆战斗部增益区的破片速度明屁增加,最大增益可达10.7%.引爆点同侧的破片速度要明显小于引爆点对侧的破片速度,方位角在0°~180°方向上,破片的速度呈递增趋势.
為研究偏心起爆子母式戰鬥部破片速度的增益,運用LS-DYNA對子母式定嚮戰鬥部變形和爆轟驅動破片飛散過程進行瞭數值模擬,模擬結果與試驗結果吻閤.結果錶明,與中心起爆相比,在與起爆位置相對的方嚮上,偏心起爆戰鬥部增益區的破片速度明屁增加,最大增益可達10.7%.引爆點同側的破片速度要明顯小于引爆點對側的破片速度,方位角在0°~180°方嚮上,破片的速度呈遞增趨勢.
위연구편심기폭자모식전두부파편속도적증익,운용LS-DYNA대자모식정향전두부변형화폭굉구동파편비산과정진행료수치모의,모의결과여시험결과문합.결과표명,여중심기폭상비,재여기폭위치상대적방향상,편심기폭전두부증익구적파편속도명비증가,최대증익가체10.7%.인폭점동측적파편속도요명현소우인폭점대측적파편속도,방위각재0°~180°방향상,파편적속도정체증추세.
To study the gain of the non-central cluster-type warhead fragments velocity, the numerical simulation of the cluster-type directional warhead detonation dispersion process was porformed by LS-DYNA. The simulated results were in good agreement with the test results. The results showed that in comparison with center priming, on the relative direction of detonation location the fragment gain speed in the eccentric warhead detonation zone increases significantly. The maximum gain achieves 10. 7 percent. The same side fragment speed of flash point was less significantly than that of opposite side fragment. When azimuth at 0°to 180° direction, the pace of fragmentation reveals an increasing trend.